| 发明名称 |
Suppression of Shock-Induced Airflow Separation |
| 摘要 |
An apparatus for suppressing shock-induced separation of high speed airflow from a relatively low-energy boundary layer. The apparatus may include an actuator or array of actuators configured to alternately inhale and exhale fluid and positioned to alternately inhale fluid from and exhale fluid into a boundary layer of a fluid mass flowing along the wall. The actuator may be positioned to inhale fluid from a boundary layer separation bubble induced by a supersonic shock wave propagated in the fluid mass. |
| 申请公布号 |
US2015027545(A1) |
申请公布日期 |
2015.01.29 |
| 申请号 |
US201313952088 |
申请日期 |
2013.07.26 |
| 申请人 |
Lockheed Martin Corporation |
发明人 |
Baruzzini Dan J.;Miller Daniel N.;Domel Neal D.;Hakes Jeff G. |
| 分类号 |
F02C7/04 |
主分类号 |
F02C7/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An apparatus for suppressing shock-induced separation of high speed airflow from a relatively low-energy boundary layer of a fluid mass flowing along a wall, the apparatus comprising an actuator configured to alternately inhale and exhale fluid, the actuator being positioned to inhale fluid from a shock-induced boundary layer separation bubble. |
| 地址 |
Bethesda MD US |
